FR3095191B1 - Système propulsif hybride et procédé de contrôle d’un tel système - Google Patents
Système propulsif hybride et procédé de contrôle d’un tel système Download PDFInfo
- Publication number
- FR3095191B1 FR3095191B1 FR1904034A FR1904034A FR3095191B1 FR 3095191 B1 FR3095191 B1 FR 3095191B1 FR 1904034 A FR1904034 A FR 1904034A FR 1904034 A FR1904034 A FR 1904034A FR 3095191 B1 FR3095191 B1 FR 3095191B1
- Authority
- FR
- France
- Prior art keywords
- electric
- hybrid propulsion
- conversion
- control
- rectifier
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 238000006243 chemical reaction Methods 0.000 abstract 3
- 238000002485 combustion reaction Methods 0.000 abstract 2
- 238000001514 detection method Methods 0.000 abstract 2
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/026—Aircraft characterised by the type or position of power plants comprising different types of power plants, e.g. combination of a piston engine and a gas-turbine
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J3/00—Circuit arrangements for ac mains or ac distribution networks
- H02J3/36—Arrangements for transfer of electric power between ac networks via a high-tension dc link
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D2221/00—Electric power distribution systems onboard aircraft
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J2310/00—The network for supplying or distributing electric power characterised by its spatial reach or by the load
- H02J2310/40—The network being an on-board power network, i.e. within a vehicle
- H02J2310/44—The network being an on-board power network, i.e. within a vehicle for aircrafts
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Power Engineering (AREA)
- Control Of Eletrric Generators (AREA)
- Electric Propulsion And Braking For Vehicles (AREA)
Abstract
L’invention concerne un système propulsif hybride (100) pour un aéronef à voilure tournante multi-rotors, comprenant : un moteur (112) à combustion interne, une machine électrique (114) accouplée au moteur à combustion interne, un redresseur (116) relié à la machine électrique, des moyens de conversion (118a, 188b, 188c, 118d), un réseau électrique (120) reliant le redresseur aux moyens de conversion, des moteurs électriques (122a, 122b, 122c, 122d) reliés aux moyens de conversion, des hélices (124a, 124b, 124c, 124d) accouplées aux moteurs électriques, Le système étant caractérisé en ce qu’il comprend : des moyens de détection configurés pour détecter une diminution d’une demande de puissance électrique au sein du système en dessous d’une valeur prédéterminée, des moyens de mise en court-circuit configurés pour court-circuiter la machine électrique lorsqu’une diminution de la demande de puissance électrique est détectée par les moyens de détection. Figure pour l'abrégé : Figure 4
Priority Applications (10)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1904034A FR3095191B1 (fr) | 2019-04-16 | 2019-04-16 | Système propulsif hybride et procédé de contrôle d’un tel système |
JP2021560271A JP2022529612A (ja) | 2019-04-16 | 2020-04-10 | ハイブリッド推進システムおよびそのようなシステムを制御するための方法 |
US17/601,816 US20220177147A1 (en) | 2019-04-16 | 2020-04-10 | Hybrid propulsion system and method for controlling such a system |
CA3132945A CA3132945A1 (fr) | 2019-04-16 | 2020-04-10 | Systeme propulsif hybride et procede de controle d'un tel systeme |
PCT/FR2020/000116 WO2020212656A1 (fr) | 2019-04-16 | 2020-04-10 | Système propulsif hybride et procédé de contrôle d'un tel système |
KR1020217034538A KR20210151846A (ko) | 2019-04-16 | 2020-04-10 | 하이브리드 추진 시스템 및 하이브리드 추진 시스템을 제어하는 방법 |
CN202080031843.1A CN113767048A (zh) | 2019-04-16 | 2020-04-10 | 混合推进***和用于控制这种***的方法 |
PL20725789.0T PL3956218T3 (pl) | 2019-04-16 | 2020-04-10 | Hybrydowy układ napędowy i sposób sterowania takim układem |
EP20725789.0A EP3956218B1 (fr) | 2019-04-16 | 2020-04-10 | Système propulsif hybride et procédé de contrôle d'un tel système |
IL287107A IL287107A (en) | 2019-04-16 | 2021-10-08 | A hybrid propulsion system and a method for controlling such a system |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1904034 | 2019-04-16 | ||
FR1904034A FR3095191B1 (fr) | 2019-04-16 | 2019-04-16 | Système propulsif hybride et procédé de contrôle d’un tel système |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3095191A1 FR3095191A1 (fr) | 2020-10-23 |
FR3095191B1 true FR3095191B1 (fr) | 2021-04-23 |
Family
ID=68072561
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1904034A Active FR3095191B1 (fr) | 2019-04-16 | 2019-04-16 | Système propulsif hybride et procédé de contrôle d’un tel système |
Country Status (10)
Country | Link |
---|---|
US (1) | US20220177147A1 (fr) |
EP (1) | EP3956218B1 (fr) |
JP (1) | JP2022529612A (fr) |
KR (1) | KR20210151846A (fr) |
CN (1) | CN113767048A (fr) |
CA (1) | CA3132945A1 (fr) |
FR (1) | FR3095191B1 (fr) |
IL (1) | IL287107A (fr) |
PL (1) | PL3956218T3 (fr) |
WO (1) | WO2020212656A1 (fr) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US11772807B2 (en) * | 2020-06-18 | 2023-10-03 | Textron Innovations Inc. | Electric distributed anti-torque architecture |
US20220135241A1 (en) * | 2020-10-30 | 2022-05-05 | Sonin Hybrid, LLC | Systems and Methods for Controlling Torque for Aerial Vehicle |
US11520361B2 (en) * | 2021-02-17 | 2022-12-06 | Rolls-Royce Singapore Pte. Ltd. | Control for a target common bus voltage |
JP2022157287A (ja) * | 2021-03-31 | 2022-10-14 | 本田技研工業株式会社 | 電力供給システム |
US20230166856A1 (en) * | 2021-11-29 | 2023-06-01 | General Electric Company | System and method for electric load control for a vehicle |
GB2613541A (en) * | 2021-11-30 | 2023-06-14 | Airbus Sas | Shielding arrangement for aircraft wiring |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CZ382892A3 (en) * | 1992-02-20 | 1993-09-15 | Asea Brown Boveri | Device with a gas turbine and method for starting thereof |
JP2003189697A (ja) * | 2001-12-19 | 2003-07-04 | Kokusan Denki Co Ltd | 交流発電機を備えた電源装置 |
EP1516424A2 (fr) * | 2002-06-18 | 2005-03-23 | Ingersoll-Rand Energy Systems Corporation | Systeme de moteur a microturbine |
CN101600882A (zh) * | 2006-01-20 | 2009-12-09 | 西南风力公司 | 风力涡轮机的失速控制器以及触发条件的控制装置 |
DE102006045731A1 (de) * | 2006-09-27 | 2008-04-03 | Zf Friedrichshafen Ag | Elektrodynamisches Antriebssystem |
KR20080001344U (ko) * | 2006-11-22 | 2008-05-27 | (주)거화테크 | 소형 풍력발전기 자동과속 방지장치 |
GB2456179B (en) * | 2008-01-07 | 2012-02-15 | Converteam Technology Ltd | Marine power distribution and propulsion systems |
CN102889181B (zh) * | 2011-01-21 | 2014-07-30 | 中科恒源科技股份有限公司 | 一种抗强风小型风力发电机 |
WO2013064928A1 (fr) * | 2011-10-31 | 2013-05-10 | Panacis Inc. | Procédé et système pour arrêter automatiquement une turbine éolienne |
US8810177B2 (en) * | 2012-09-12 | 2014-08-19 | GM Global Technology Operations LLC | System and method for implementing a remedial electrical short |
CN104791192B (zh) * | 2015-04-16 | 2018-02-27 | 深圳市风光宝新能源科技有限公司 | 一种风力机限速与刹车保护控制的装置及方法 |
FR3056555B1 (fr) * | 2016-09-29 | 2018-12-07 | Safran Helicopter Engines | Systeme propulsif hybride pour aeronef a voilure tournante multirotor comprenant des moyens ameliores de conversion dc/ac |
WO2018175349A1 (fr) * | 2017-03-19 | 2018-09-27 | Zunum Aero, Inc. | Aéronef hybride-électrique, et procédés, appareil et systèmes destinés à faciliter ledit aéronef |
CN106877478B (zh) * | 2017-04-28 | 2020-03-27 | 重庆三信电子股份有限公司 | 一种车用电源***及有源混合整流器和控制方法 |
-
2019
- 2019-04-16 FR FR1904034A patent/FR3095191B1/fr active Active
-
2020
- 2020-04-10 KR KR1020217034538A patent/KR20210151846A/ko unknown
- 2020-04-10 CN CN202080031843.1A patent/CN113767048A/zh active Pending
- 2020-04-10 EP EP20725789.0A patent/EP3956218B1/fr active Active
- 2020-04-10 JP JP2021560271A patent/JP2022529612A/ja active Pending
- 2020-04-10 CA CA3132945A patent/CA3132945A1/fr active Pending
- 2020-04-10 PL PL20725789.0T patent/PL3956218T3/pl unknown
- 2020-04-10 WO PCT/FR2020/000116 patent/WO2020212656A1/fr unknown
- 2020-04-10 US US17/601,816 patent/US20220177147A1/en active Pending
-
2021
- 2021-10-08 IL IL287107A patent/IL287107A/en unknown
Also Published As
Publication number | Publication date |
---|---|
CA3132945A1 (fr) | 2020-10-22 |
US20220177147A1 (en) | 2022-06-09 |
PL3956218T3 (pl) | 2023-12-11 |
EP3956218A1 (fr) | 2022-02-23 |
CN113767048A (zh) | 2021-12-07 |
WO2020212656A1 (fr) | 2020-10-22 |
FR3095191A1 (fr) | 2020-10-23 |
IL287107A (en) | 2021-12-01 |
KR20210151846A (ko) | 2021-12-14 |
EP3956218B1 (fr) | 2023-08-30 |
JP2022529612A (ja) | 2022-06-23 |
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